Composite Barrel Sections for Aircraft Fuselages and Other Structures
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Accused Products
Abstract
Composite sections for aircraft fuselages and methods and systems for manufacturing such sections are herein. A composite aircraft panel manufacturing assembly comprises a skin, a stiffener, a tubular bladder, and at least one ply of fabric. The stiffener comprises first and second flange portions bonded to the skin. The stiffener further comprises an interior surface, spaced apart from the skin, and extending between the first and second flange portions. The tubular bladder extends longitudinally between the interior surface of the stiffener and the skin. The at least one ply of fabric extends around the bladder and is bonded to the interior surface of the stiffener and an adjacent portion of the skin between the first and second flange portions.
13 Citations
66 Claims
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1-62. -62. (canceled)
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63. A composite aircraft panel manufacturing assembly comprising:
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a skin; a stiffener having first and second flange portions bonded to the skin, the stiffener further including an interior surface extending between the first and second flange portions, wherein the interior surface is spaced apart from the skin and at least a portion of the interior surface faces toward the skin; a tubular bladder extending longitudinally between the interior surface of the stiffener and the skin; and at least one ply of fabric extending around the bladder and bonded to the interior surface of the stiffener and an adjacent portion of the skin between the first and second flange portions. - View Dependent Claims (64, 65, 66)
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Specification